ATE511130T1 - Verfahren zur erzeugung von variabler schubverringerung während des abflugs eines flugzeuges - Google Patents
Verfahren zur erzeugung von variabler schubverringerung während des abflugs eines flugzeugesInfo
- Publication number
- ATE511130T1 ATE511130T1 AT08731639T AT08731639T ATE511130T1 AT E511130 T1 ATE511130 T1 AT E511130T1 AT 08731639 T AT08731639 T AT 08731639T AT 08731639 T AT08731639 T AT 08731639T AT E511130 T1 ATE511130 T1 AT E511130T1
- Authority
- AT
- Austria
- Prior art keywords
- aircraft
- sound exposure
- airspeed
- altitude
- departure
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
- Navigation (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US89480307P | 2007-03-14 | 2007-03-14 | |
US11/954,056 US8670881B2 (en) | 2007-03-14 | 2007-12-11 | Flight management system for generating variable thrust cutback during aircraft departure |
PCT/US2008/056174 WO2008112530A2 (en) | 2007-03-14 | 2008-03-07 | Flight management system for generating variable thrust cutback during aircraft departure |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE511130T1 true ATE511130T1 (de) | 2011-06-15 |
Family
ID=39712182
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT08731639T ATE511130T1 (de) | 2007-03-14 | 2008-03-07 | Verfahren zur erzeugung von variabler schubverringerung während des abflugs eines flugzeuges |
Country Status (7)
Country | Link |
---|---|
US (1) | US8670881B2 (de) |
EP (1) | EP2135147B1 (de) |
JP (1) | JP5292315B2 (de) |
AT (1) | ATE511130T1 (de) |
BR (1) | BRPI0807287B1 (de) |
CA (1) | CA2680287C (de) |
WO (1) | WO2008112530A2 (de) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2912243B1 (fr) * | 2007-02-07 | 2009-03-13 | Airbus France Sas | Dispositif et procede d'aide a la gestion d'une panne moteur d'un aeronef |
US8380371B2 (en) * | 2007-03-14 | 2013-02-19 | General Electric Company | Method of generating variable thrust cutback during aircraft departure |
NL2002064C (nl) * | 2008-10-07 | 2010-04-08 | Robertus Gerardus De Boer | Gedifferentieerde stuwkracht startmethode voor een vliegtuig. |
PT104972B (pt) | 2010-02-19 | 2017-10-25 | Inst Superior Técnico | Turbina com rotor de entrada e saída radiais para aplicações em escoamentos bidireccionados |
US8909395B2 (en) | 2011-04-29 | 2014-12-09 | Airbus Engineering Centre India | System and method for aircraft performance predictions for climb flight phase |
FR2975486B1 (fr) | 2011-05-20 | 2015-05-29 | Eurocopter France | Dispositif et procede de construction de route aerienne pour atteindre une destination |
US8742973B1 (en) * | 2011-09-22 | 2014-06-03 | Rockwell Collins, Inc. | System and method of determining increased turbulence susceptibility with elapsed flight time |
GB201204925D0 (en) * | 2012-01-24 | 2012-05-02 | Airbus Operations Ltd | System and method for providing an aircraft noise advisory during departure and arrival of an aircraft |
CA2804120C (en) | 2013-01-29 | 2020-03-31 | Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defence | Vehicle noise detectability calculator |
FR3013880B1 (fr) | 2013-11-26 | 2017-03-31 | Airbus Operations Sas | Systeme avionique, notamment un systeme de gestion de vol d'un aeronef |
US10112722B2 (en) | 2015-01-15 | 2018-10-30 | Unison Industries Llc | Power control for propeller-driven aircraft |
US9696724B1 (en) * | 2016-04-22 | 2017-07-04 | Rockwell Collins, Inc. | Takeoff automating system, device, and method |
US10796585B2 (en) * | 2017-06-12 | 2020-10-06 | United States Of America As Represented By The Administrator Of Nasa | Device for providing real-time rotorcraft noise abatement information |
US10671092B2 (en) | 2017-10-20 | 2020-06-02 | The Boeing Company | Airplane climb thrust optimization |
US11216011B2 (en) | 2018-03-16 | 2022-01-04 | Embraer S.A. | Optimized trajectory to noise improvement with auto-takeoff |
US11391218B2 (en) * | 2019-03-22 | 2022-07-19 | Pratt & Whitney Canada Corp. | Method and system for setting power of an aircraft engine |
US11591075B2 (en) | 2019-06-13 | 2023-02-28 | Hamilton Sundstrand Corporation | Intelligent engine offload of auxiliary loads for enhanced engine durability |
US11733712B2 (en) * | 2020-07-03 | 2023-08-22 | Honeywell International Inc. | Systems and methods for generating displays for noise abatement departure procedures |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1156324A (en) * | 1965-07-14 | 1969-06-25 | Elliott Brothers London Ltd | Improvements relating to Take-Off Director Systems for Aircraft |
US4019702A (en) * | 1975-11-13 | 1977-04-26 | The Boeing Company | Method and apparatus for guiding a jet aircraft in a noise-abated post-takeoff climb |
US5121325A (en) * | 1990-04-04 | 1992-06-09 | Smiths Industries Aerospace & Defense Systems, Inc. | Required time of arrival (RTA) control system |
US5299765A (en) * | 1991-12-23 | 1994-04-05 | The Boeing Company | Apparatus and methods for controlling aircraft thrust during a climb |
US5752216A (en) * | 1994-07-06 | 1998-05-12 | Dimensions International, Inc. | Non-intrusive data interface system for air traffic control |
JP2736045B2 (ja) | 1996-03-19 | 1998-04-02 | 株式会社コミュータヘリコプタ先進技術研究所 | ヘリコプタの低騒音着陸装置 |
JP2968511B2 (ja) * | 1998-03-25 | 1999-10-25 | 株式会社コミュータヘリコプタ先進技術研究所 | ヘリコプタの低騒音着陸装置および低騒音着陸システム |
US6880784B1 (en) * | 2003-05-08 | 2005-04-19 | Supersonic Aerospace International, Llc | Automatic takeoff thrust management system |
US6905091B2 (en) * | 2003-07-14 | 2005-06-14 | Supersonic Aerospace International, Llc | System and method for controlling the acoustic signature of a device |
JP4491586B2 (ja) * | 2004-08-06 | 2010-06-30 | 独立行政法人 宇宙航空研究開発機構 | 低騒音飛行支援システム |
US7584028B2 (en) * | 2006-11-14 | 2009-09-01 | The Boeing Company | Methods and systems for implementing location based noise abatement procedures |
US7599805B2 (en) * | 2007-03-12 | 2009-10-06 | Lockheed-Martin Corporation | Systems and methods for predicting supersonic acoustic signatures |
US8380371B2 (en) * | 2007-03-14 | 2013-02-19 | General Electric Company | Method of generating variable thrust cutback during aircraft departure |
US8131410B2 (en) * | 2007-06-15 | 2012-03-06 | The Boeing Company | Quiet climb crew interface |
-
2007
- 2007-12-11 US US11/954,056 patent/US8670881B2/en active Active
-
2008
- 2008-03-07 WO PCT/US2008/056174 patent/WO2008112530A2/en active Application Filing
- 2008-03-07 AT AT08731639T patent/ATE511130T1/de not_active IP Right Cessation
- 2008-03-07 EP EP08731639A patent/EP2135147B1/de active Active
- 2008-03-07 BR BRPI0807287-6A patent/BRPI0807287B1/pt not_active IP Right Cessation
- 2008-03-07 CA CA2680287A patent/CA2680287C/en not_active Expired - Fee Related
- 2008-03-07 JP JP2009553700A patent/JP5292315B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
BRPI0807287A2 (pt) | 2014-05-06 |
JP2010521359A (ja) | 2010-06-24 |
BRPI0807287B1 (pt) | 2018-08-07 |
CA2680287C (en) | 2015-04-28 |
EP2135147B1 (de) | 2011-05-25 |
WO2008112530A2 (en) | 2008-09-18 |
US20090132106A1 (en) | 2009-05-21 |
EP2135147A2 (de) | 2009-12-23 |
JP5292315B2 (ja) | 2013-09-18 |
WO2008112530A3 (en) | 2009-10-22 |
US8670881B2 (en) | 2014-03-11 |
CA2680287A1 (en) | 2008-09-18 |
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